FR1526647A - Advanced central body propellant nozzles - Google Patents
Advanced central body propellant nozzlesInfo
- Publication number
- FR1526647A FR1526647A FR5119A FR38005119A FR1526647A FR 1526647 A FR1526647 A FR 1526647A FR 5119 A FR5119 A FR 5119A FR 38005119 A FR38005119 A FR 38005119A FR 1526647 A FR1526647 A FR 1526647A
- Authority
- FR
- France
- Prior art keywords
- central body
- body propellant
- advanced central
- propellant nozzles
- nozzles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/04—Mounting of an exhaust cone in the jet pipe
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US554952A US3402894A (en) | 1966-06-01 | 1966-06-01 | Base-thrust nozzles |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1526647A true FR1526647A (en) | 1968-05-24 |
Family
ID=24215382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR5119A Expired FR1526647A (en) | 1966-06-01 | 1967-06-01 | Advanced central body propellant nozzles |
Country Status (4)
Country | Link |
---|---|
US (1) | US3402894A (en) |
DE (1) | DE1626143A1 (en) |
FR (1) | FR1526647A (en) |
GB (1) | GB1194716A (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3527407A (en) * | 1968-07-23 | 1970-09-08 | United Aircraft Corp | Base-thrust nozzle |
US3888419A (en) * | 1971-09-13 | 1975-06-10 | Thiokol Corp | Spike nozzle for rockets |
US3989191A (en) * | 1971-09-13 | 1976-11-02 | Thiokol Corporation | Thrust control nozzle for rockets |
US4168031A (en) * | 1971-09-13 | 1979-09-18 | Thiokol Corporation | Thrust control nozzle for rockets |
US3885385A (en) * | 1972-12-22 | 1975-05-27 | Us Army | Base drag reduction |
US3848806A (en) * | 1973-04-30 | 1974-11-19 | Rockwell International Corp | Throttling venturi valve |
US4567960A (en) * | 1982-08-23 | 1986-02-04 | The Boeing Company | Fixed geometry controlled entrainment ventilated convergent nozzle and method |
DE3578781D1 (en) * | 1985-11-26 | 1990-08-23 | Boeing Co | SILENCER WITH FIXED GEOMETRY FOR A JET ENGINE. |
US4782660A (en) * | 1987-01-20 | 1988-11-08 | Rockwell International Corporation | Sequenced and pressure controlled injector |
US7823376B2 (en) * | 2005-09-13 | 2010-11-02 | Aerojet-General Corporation | Thrust augmentation in plug nozzles and expansion-deflection nozzles |
FR2970465B1 (en) * | 2011-01-19 | 2013-10-11 | Aircelle Sa | NACELLE FOR A DOUBLE FLOW AIRCRAFT AIRCRAFT TURBOREACTOR. |
DE102017130568A1 (en) * | 2017-12-19 | 2019-06-19 | Rolls-Royce Deutschland Ltd & Co Kg | Discharge nozzle for a turbofan engine of a supersonic aircraft |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2663140A (en) * | 1946-08-23 | 1953-12-22 | Lockheed Aircraft Corp | Fuel system for ram jets |
US2793493A (en) * | 1950-04-28 | 1957-05-28 | Snecma | Devices for deflecting fluid jets |
US3048974A (en) * | 1952-04-23 | 1962-08-14 | Snecma | Jet deflecting device for jet propulsion units |
FR1130131A (en) * | 1955-07-12 | 1957-01-31 | Snecma | Improvement in the control of stator-reactor or annular wing aerodynes |
US2957307A (en) * | 1956-11-06 | 1960-10-25 | Amcel Propulsion Inc | Powder propellant rocket motors |
FR1268781A (en) * | 1960-09-26 | 1961-08-04 | Olin Mathieson | Rocket motor and method of adjusting the thrust of a rocket motor |
GB1051666A (en) * | 1962-01-10 | 1900-01-01 | ||
US3296799A (en) * | 1965-08-27 | 1967-01-10 | Thiokol Chemical Corp | Thrust vector control system |
-
1966
- 1966-06-01 US US554952A patent/US3402894A/en not_active Expired - Lifetime
-
1967
- 1967-05-31 GB GB25197/67A patent/GB1194716A/en not_active Expired
- 1967-05-31 DE DE19671626143 patent/DE1626143A1/en not_active Withdrawn
- 1967-06-01 FR FR5119A patent/FR1526647A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3402894A (en) | 1968-09-24 |
GB1194716A (en) | 1970-06-10 |
DE1626143A1 (en) | 1970-09-24 |
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